<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE ep-patent-document PUBLIC "-//EPO//EP PATENT DOCUMENT 1.4//EN" "ep-patent-document-v1-4.dtd"><!-- Disclaimer: This ST.36 XML data has been generated from SGML data available on ESPACE discs EPAS Volumes 2003/201 to 203 enriched by the abstract retrieved from the corresponding A2/A1 document - March 2013 - EPO - Dir. Publication - kbaumeister@epo.org --><ep-patent-document id="EP84308736A3" lang="en" country="EP" doc-number="0147987" date-publ="19860820" file="84308736" kind="A3" status="n" dtd-version="ep-patent-document-v1-4"><SDOBI lang="en"><B000><eptags><B001EP>DEFRGBITSE</B001EP></eptags></B000><B100><B110>0147987</B110><B120><B121>EUROPEAN PATENT APPLICATION</B121></B120><B130>A3</B130><B140><date>19860820</date></B140><B190>EP</B190></B100><B200><B210>84308736</B210><B220><date>19841214</date></B220></B200><B300><B310>562488</B310><B320><date>19831216</date></B320><B330><ctry>US</ctry></B330><B310>562490</B310><B320><date>19831216</date></B320><B330><ctry>US</ctry></B330></B300><B400><B405><date>19860820</date><bnum>198634</bnum></B405><B430><date>19850710</date><bnum>198528</bnum></B430></B400><B500><B510><B511> 6F 25B  09/00   A</B511><B512> 6F 25B  11:00   B</B512><B512> 6B 64D  13:08   B</B512><B512> 6F 04D  25:16   B</B512></B510><B540><B541>en</B541><B542>Turbine-heat exchanger assembly</B542><B541>fr</B541><B542>Montage de turbine et d'échangeur de chaleur</B542><B541>de</B541><B542>Zusammenbau einer Turbine und eines Wärmetauscher</B542></B540></B500><B700><B710><B711><snm>THE GARRETT CORPORATION</snm></B711></B710><B720><B721><snm>Wieland, K.H.</snm></B721><B721><snm>Spencer, D.M.</snm></B721><B721><snm>Kinsell, R.C.</snm></B721></B720></B700><B800><B840><ctry>DE</ctry><ctry>FR</ctry><ctry>GB</ctry><ctry>IT</ctry><ctry>SE</ctry></B840><B880><date>19860820</date><bnum>198634</bnum></B880></B800></SDOBI><abstract id="abst" lang="en"><p id="pa01" num="0001">A compact air cycle refrigeration system utilizes a three wheel air cycle cooling machine having a fan mounted between a turbine and compressor on a common drive shaft. The fan is positioned between two series-mounted heat exchangers mounted in a ram air duct and used to cool hot engine bleed air which drives the turbine. The turbine, in turn, drives the fan and the compressor, and the eingine bleed air is directed, via the compressor, through the heat exchangers and into the turbine.<!-- EPO <DP n="2"> --><img id="iaf01" file="imgaf001.tif" wi="126" he="92" img-content="drawing" img-format="tif" inline="no" /></p></abstract><search-report-data lang="en" id="srep" srep-office="EP" date-produced=""><doc-page id="srep0001" file="srep0001.tif" type="tif" orientation="portrait" he="295" wi="208" /><doc-page id="srep0002" file="srep0002.tif" type="tif" orientation="portrait" he="295" wi="208" /></search-report-data></ep-patent-document>